Date: May 21st 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 127)
---------------------------------------

Vector Time (GMT): 2009/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1847138
15                 A    =         6730584
14  meter
 Y    =        5526828
65  meter          E    =           
0011868
 Z    =       -3364537
54                 I    =           51
96953
 XDOT =      -4338
646868                 Wp   =           38
36639
 YDOT =       4293
917363  meter/sec      RA   =           98
36527  deg
 ZDOT =       4689
419519                 TA   =          282
22912
                                          MA   =          282
36201
                                          Ha   =            194
475  n
mi
                                          Hp   =            183
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6060164
52                 X    =         1801543
39
 Y    =       18132639
92  feet           Y    =         5547229
70  meter
 Z    =      -11038508
99                 Z    =        -3355674
47
 XDOT =     -14234
405734                 XDOT =       -4409
120274
 YDOT =      14087
655389  feet/sec       YDOT =        4245
005752  meter/sec
 ZDOT =      15385
234643                 ZDOT =        4668
171265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18415963
95                 X    =         5613185
81
 Y    =        5209882
35  feet           Y    =         1587972
14  meter
 Z    =      -11003467
76                 Z    =        -3353856
97
 XDOT =       3891
783189                 XDOT =        1186
215516
 YDOT =      18438
197901  feet/sec       YDOT =        5619
962720  meter/sec
 ZDOT =      15302
293189                 ZDOT =        4664
138964


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09138
50696387  
00010596  00000-0  82463-4 0  9005
2 25544  51
6372  99
1545 0009539  15
4625 344
6827 15
72841106  1288


Satellite: ISS
Catalog Number: 25544
Epoch time:      09138
50696387   =   yrday
fracday
Element set:     900
Inclination:       51
6372  deg
RA of node:        99
1545  deg
Eccentricity:     
0009539     
Arg of perigee:    15
4625  deg
Mean anomaly:     344
6827  deg
Mean motion:   15
72841106  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             128
Checksum:              323


Coasting Arc #2 (Orbit 143)
---------------------------------------

Vector Time (GMT): 2009/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3292229
53                 A    =         6728863
70  meter
 Y    =       -4421306
80  meter          E    =           
0014227
 Z    =       -3875448
64                 I    =           51
96813
 XDOT =       2905
215148                 Wp   =           40
93132
 YDOT =       5790
142734  meter/sec      RA   =           93
31191  deg
 ZDOT =      -4135
699012                 TA   =          185
96917
                                          MA   =          185
98615
                                          Ha   =            194
425  n
mi
                                          Hp   =            183
713

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10801277
98                 X    =         3360251
12
 Y    =      -14505599
73  feet           Y    =        -4384110
61  meter
 Z    =      -12714726
50                 Z    =        -3859289
81
 XDOT =       9531
545760                 XDOT =        2860
343612
 YDOT =      18996
531281  feet/sec       YDOT =        5822
379899  meter/sec
 ZDOT =     -13568
566311                 ZDOT =       -4121
693947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6102204
45                 X    =        -1859951
92
 Y    =      -17071658
02  feet           Y    =        -5203441
36  meter
 Z    =      -12651715
03                 Z    =        -3856242
74
 XDOT =      19901
199908                 XDOT =        6065
885732
 YDOT =       2905
917792  feet/sec       YDOT =         885
723743  meter/sec
 ZDOT =     -13513
379883                 ZDOT =       -4118
878188


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09139
52352214  
00010596  00000-0  82463-4 0  9017
2 25544  51
6380  93
9419 0009539  19
1677 340
9843 15
72902011  1445


Satellite: ISS
Catalog Number: 25544
Epoch time:      09139
52352214   =   yrday
fracday
Element set:     901
Inclination:       51
6380  deg
RA of node:        93
9419  deg
Eccentricity:     
0009539     
Arg of perigee:    19
1677  deg
Mean anomaly:     340
9843  deg
Mean motion:   15
72902011  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             144
Checksum:              302


Coasting Arc #3 (Orbit 159)
---------------------------------------

Vector Time (GMT): 2009/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3161364
92                 A    =         6728828
08  meter
 Y    =       -4516227
06  meter          E    =           
0018212
 Z    =        3854017
54                 I    =           51
96910
 XDOT =       3066
645212                 Wp   =           54
82267
 YDOT =      -5711
731783  meter/sec      RA   =           88
15643  deg
 ZDOT =      -4153
666023                 TA   =           78
50694
                                          MA   =           78
30249
                                          Ha   =            194
488  n
mi
                                          Hp   =            183
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10371932
16                 X    =        -3129351
20
 Y    =      -14817017
91  feet           Y    =        -4551400
54  meter
 Z    =       12644414
49                 Z    =         3838736
83
 XDOT =      10061
171954                 XDOT =        3150
464952
 YDOT =     -18739
277504  feet/sec       YDOT =       -5676
969840  meter/sec
 ZDOT =     -13627
513200                 ZDOT =       -4138
564760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18108305
78                 X    =        -5519411
60
 Y    =         852348
97  feet           Y    =          259795
97  meter
 Z    =       12584314
73                 Z    =         3835699
13
 XDOT =     -10298
654213                 XDOT =       -3139
029804
 YDOT =     -17297
807413  feet/sec       YDOT =       -5272
371699  meter/sec
 ZDOT =     -13568
710161                 ZDOT =       -4135
742857


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09140
54006051  
00010596  00000-0  82463-4 0  9027
2 25544  51
6383  88
7298 0009516  22
4711 337
6866 15
72932842  1607


Satellite: ISS
Catalog Number: 25544
Epoch time:      09140
54006051   =   yrday
fracday
Element set:     902
Inclination:       51
6383  deg
RA of node:        88
7298  deg
Eccentricity:     
0009516     
Arg of perigee:    22
4711  deg
Mean anomaly:     337
6866  deg
Mean motion:   15
72932842  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             160
Checksum:              304


Coasting Arc #4 (Orbit 175)
---------------------------------------

Vector Time (GMT): 2009/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1987749
84                 A    =         6730244
50  meter
 Y    =        5466391
58  meter          E    =           
0018836
 Z    =        3362616
75                 I    =           51
97254
 XDOT =      -4227
205984                 Wp   =           62
94087
 YDOT =      -4427
051134  meter/sec      RA   =           83
10340  deg
 ZDOT =       4686
392512                 TA   =          336
50672
                                          MA   =          336
59266
                                          Ha   =            194
521  n
mi
                                          Hp   =            183
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6521488
99                 X    =        -2065063
56
 Y    =       17934355
59  feet           Y    =         5443730
85  meter
 Z    =       11032207
18                 Z    =         3352772
69
 XDOT =     -13868
786036                 XDOT =       -4200
153914
 YDOT =     -14524
445978  feet/sec       YDOT =       -4474
171339  meter/sec
 ZDOT =      15375
303516                 ZDOT =        4665
921654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11850571
75                 X    =         3612054
27
 Y    =       14985899
91  feet           Y    =         4567702
29  meter
 Z    =       10993965
51                 Z    =         3350960
69
 XDOT =     -18584
084462                 XDOT =       -5664
428944
 YDOT =       3447
414218  feet/sec       YDOT =        1050
771854  meter/sec
 ZDOT =      15294
891753                 ZDOT =        4661
883006


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09141
55657888  
00010596  00000-0  82463-4 0  9030
2 25544  51
6389  83
5177 0009418  26
5239 333
6404 15
72962552  1765


Satellite: ISS
Catalog Number: 25544
Epoch time:      09141
55657888   =   yrday
fracday
Element set:     903
Inclination:       51
6389  deg
RA of node:        83
5177  deg
Eccentricity:     
0009418     
Arg of perigee:    26
5239  deg
Mean anomaly:     333
6404  deg
Mean motion:   15
72962552  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             176
Checksum:              335


Coasting Arc #5 (Orbit 190)
---------------------------------------

Vector Time (GMT): 2009/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4112163
26                 A    =         6727148
48  meter
 Y    =        3151433
53  meter          E    =           
0013721
 Z    =       -4298628
45                 I    =           51
95783
 XDOT =      -1416
854124                 Wp   =           67
49580
 YDOT =       6674
218094  meter/sec      RA   =           77
94869  deg
 ZDOT =       3551
722604                 TA   =          238
33171
                                          MA   =          238
46561
                                          Ha   =            194
565  n
mi
                                          Hp   =            183
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13491349
28                 X    =         4097500
24
 Y    =       10339348
85  feet           Y    =         3197336
61  meter
 Z    =      -14103111
72                 Z    =        -4278686
36
 XDOT =      -4648
471535                 XDOT =       -1508
635096
 YDOT =      21897
040992  feet/sec       YDOT =        6657
860453  meter/sec
 ZDOT =      11652
633215                 ZDOT =        3544
617126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15798994
09                 X    =         4815533
40
 Y    =       -6442969
36  feet           Y    =        -1963817
06  meter
 Z    =      -14024846
95                 Z    =        -4274773
35
 XDOT =      15999
821024                 XDOT =        4876
745448
 YDOT =      14029
442599  feet/sec       YDOT =        4276
174104  meter/sec
 ZDOT =      11625
168179                 ZDOT =        3543
351261


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09142
50954720  
00010596  00000-0  82463-4 0  9042
2 25544  51
6393  78
6311 0009468  29
5790 330
5906 15
72980116  1911


Satellite: ISS
Catalog Number: 25544
Epoch time:      09142
50954720   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:        78
6311  deg
Eccentricity:     
0009468     
Arg of perigee:    29
5790  deg
Mean anomaly:     330
5906  deg
Mean motion:   15
72980116  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             191
Checksum:              313


Coasting Arc #6 (Orbit 206)
---------------------------------------

Vector Time (GMT): 2009/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         470842
44                 A    =         6731402
55  meter
 Y    =       -6081661
62  meter          E    =           
0011041
 Z    =       -2862515
88                 I    =           51
96639
 XDOT =       5031
970352                 Wp   =           57
89305
 YDOT =       2786
185139  meter/sec      RA   =           72
89126  deg
 ZDOT =      -5100
335952                 TA   =          154
74680
                                          MA   =          154
69278
                                          Ha   =            194
528  n
mi
                                          Hp   =            182
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1544758
65                 X    =          552719
53
 Y    =      -19952958
08  feet           Y    =        -6075938
19  meter
 Z    =       -9391456
29                 Z    =        -2860030
42
 XDOT =      16509
089082                 XDOT =        5025
217874
 YDOT =       9141
027360  feet/sec       YDOT =        2842
418518  meter/sec
 ZDOT =     -16733
385670                 ZDOT =       -5075
906064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16572969
58                 X    =        -5051441
13
 Y    =      -11225877
46  feet           Y    =        -3421647
45  meter
 Z    =       -9382037
16                 Z    =        -2859644
93
 XDOT =      15319
396840                 XDOT =        4669
352157
 YDOT =      -8734
862714  feet/sec       YDOT =       -2662
386155  meter/sec
 ZDOT =     -16637
568061                 ZDOT =       -5071
130745


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09143
52602702  
00010596  00000-0  82463-4 0  9056
2 25544  51
6404  73
4185 0009501  33
5092 326
6670 15
73024916  2074


Satellite: ISS
Catalog Number: 25544
Epoch time:      09143
52602702   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:        73
4185  deg
Eccentricity:     
0009501     
Arg of perigee:    33
5092  deg
Mean anomaly:     326
6670  deg
Mean motion:   15
73024916  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             207
Checksum:              280


Coasting Arc #7 (Orbit 222)
---------------------------------------

Vector Time (GMT): 2009/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4591344
81                 A    =         6725764
79  meter
 Y    =       -1688747
66  meter          E    =           
0017345
 Z    =        4609558
49                 I    =           51
93764
 XDOT =       -390
909196                 Wp   =           50
07569
 YDOT =      -7096
354571  meter/sec      RA   =           67
74019  deg
 ZDOT =      -2970
949207                 TA   =           69
34832
                                          MA   =           69
16242
                                          Ha   =            194
648  n
mi
                                          Hp   =            182
764

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15063467
24                 X    =        -4594512
57
 Y    =       -5540510
69  feet           Y    =        -1740109
24  meter
 Z    =       15123223
38                 Z    =         4587245
29
 XDOT =      -1282
510486                 XDOT =        -297
094877
 YDOT =     -23282
003185  feet/sec       YDOT =       -7100
200903  meter/sec
 ZDOT =      -9747
208685                 ZDOT =       -2972
621596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12106507
48                 X    =        -3690063
48
 Y    =       10661889
53  feet           Y    =         3249743
93  meter
 Z    =       15035749
98                 Z    =         4582896
59
 XDOT =     -20260
508273                 XDOT =       -6175
402922
 YDOT =      -9165
317814  feet/sec       YDOT =       -2793
588870  meter/sec
 ZDOT =      -9754
110126                 ZDOT =       -2973
052767


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09144
54248715  
00010596  00000-0  82463-4 0  9060
2 25544  51
6405  68
2066 0009449  37
2571 322
9246 15
73043314  2238


Satellite: ISS
Catalog Number: 25544
Epoch time:      09144
54248715   =   yrday
fracday
Element set:     906
Inclination:       51
6405  deg
RA of node:        68
2066  deg
Eccentricity:     
0009449     
Arg of perigee:    37
2571  deg
Mean anomaly:     322
9246  deg
Mean motion:   15
73043314  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             223
Checksum:              298


Coasting Arc #8 (Orbit 238)
---------------------------------------

Vector Time (GMT): 2009/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1164599
44                 A    =         6732504
85  meter
 Y    =        6200372
87  meter          E    =           
0022538
 Z    =        2314317
49                 I    =           51
94866
 XDOT =      -5345
525743                 Wp   =           59
79981
 YDOT =      -1042
830049  meter/sec      RA   =           62
67564  deg
 ZDOT =       5455
773741                 TA   =          326
13534
                                          MA   =          326
27905
                                          Ha   =            194
592  n
mi
                                          Hp   =            182
579

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3820864
32                 X    =         1083936
57
 Y    =       20342430
68  feet           Y    =         6212944
66  meter
 Z    =        7592905
16                 Z    =         2319780
43
 XDOT =     -17537
814118                 XDOT =       -5359
970894
 YDOT =      -3421
358429  feet/sec       YDOT =       -1102
688629  meter/sec
 ZDOT =      17899
520147                 ZDOT =        5429
769507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19781788
57                 X    =         6029489
16
 Y    =        6063367
78  feet           Y    =         1848114
50  meter
 Z    =        7614598
53                 Z    =         2320929
63
 XDOT =     -10752
624684                 XDOT =       -3277
400004
 YDOT =      12614
350946  feet/sec       YDOT =        3844
854168  meter/sec
 ZDOT =      17797
616323                 ZDOT =        5424
713455


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09145
55892740  
00010596  00000-0  82463-4 0  9076
2 25544  51
6409  62
9940 0009463  40
8429 319
3441 15
73064582  2396


Satellite: ISS
Catalog Number: 25544
Epoch time:      09145
55892740   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:        62
9940  deg
Eccentricity:     
0009463     
Arg of perigee:    40
8429  deg
Mean anomaly:     319
3441  deg
Mean motion:   15
73064582  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             239
Checksum:              322


Coasting Arc #9 (Orbit 253)
---------------------------------------

Vector Time (GMT): 2009/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4634124
79                 A    =         6724502
26  meter
 Y    =         150074
25  meter          E    =           
0018409
 Z    =       -4884758
18                 I    =           51
90792
 XDOT =       2244
842819                 Wp   =           79
79590
 YDOT =       6965
002718  meter/sec      RA   =           57
52854  deg
 ZDOT =       2354
303564                 TA   =          213
04757
                                          MA   =          213
16274
                                          Ha   =            194
586  n
mi
                                          Hp   =            182
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15203821
48                 X    =         4655831
66
 Y    =         492369
59  feet           Y    =          202018
05  meter
 Z    =      -16026109
51                 Z    =        -4862192
67
 XDOT =       7364
969880                 XDOT =        2155
355275
 YDOT =      22851
058785  feet/sec       YDOT =        6989
605055  meter/sec
 ZDOT =       7724
093059                 ZDOT =        2364
993071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7282838
87                 X    =         2219809
29
 Y    =      -13460477
81  feet           Y    =        -4102753
64  meter
 Z    =      -15937709
89                 Z    =        -4857813
97
 XDOT =      22730
285338                 XDOT =        6928
190971
 YDOT =       3144
349708  feet/sec       YDOT =         958
397791  meter/sec
 ZDOT =       7766
289167                 ZDOT =        2367
164938


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09146
51182107  
00010596  00000-0  82463-4 0  9083
2 25544  51
6416  58
1072 0009408  44
1084 316
0828 15
73104527  2544


Satellite: ISS
Catalog Number: 25544
Epoch time:      09146
51182107   =   yrday
fracday
Element set:     908
Inclination:       51
6416  deg
RA of node:        58
1072  deg
Eccentricity:     
0009408     
Arg of perigee:    44
1084  deg
Mean anomaly:     316
0828  deg
Mean motion:   15
73104527  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             254
Checksum:              287


Coasting Arc #10 (Orbit 269)
---------------------------------------

Vector Time (GMT): 2009/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2720211
71                 A    =         6733202
38  meter
 Y    =       -5886012
13  meter          E    =           
0011407
 Z    =       -1825312
64                 I    =           51
92084
 XDOT =       5140
957329                 Wp   =           87
06361
 YDOT =       -621
846693  meter/sec      RA   =           52
45409  deg
 ZDOT =      -5685
978950                 TA   =          113
07170
                                          MA   =          112
95140
                                          Ha   =            194
532  n
mi
                                          Hp   =            182
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8924579
11                 X    =        -2645324
11
 Y    =      -19311063
41  feet           Y    =        -5916012
07  meter
 Z    =       -5988558
52                 Z    =        -1838346
61
 XDOT =      16866
657905                 XDOT =        5175
150333
 YDOT =      -2040
179439  feet/sec       YDOT =        -564
165293  meter/sec
 ZDOT =     -18654
786583                 ZDOT =       -5660
921193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21256620
73                 X    =        -6479018
00
 Y    =        -322406
27  feet           Y    =          -98269
43  meter
 Z    =       -6039887
81                 Z    =        -1840957
80
 XDOT =       5467
235491                 XDOT =        1666
413378
 YDOT =     -14640
986865  feet/sec       YDOT =       -4462
572796  meter/sec
 ZDOT =     -18556
652311                 ZDOT =       -5656
067624


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09147
52822241  
00010596  00000-0  82463-4 0  9096
2 25544  51
6419  52
8940 0009275  47
9764 312
2187 15
73119978  2700


Satellite: ISS
Catalog Number: 25544
Epoch time:      09147
52822241   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:        52
8940  deg
Eccentricity:     
0009275     
Arg of perigee:    47
9764  deg
Mean anomaly:     312
2187  deg
Mean motion:   15
73119978  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             270
Checksum:              326


Coasting Arc #11 (Orbit 285)
---------------------------------------

Vector Time (GMT): 2009/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4263137
92                 A    =         6723449
74  meter
 Y    =        1220542
77  meter          E    =           
0014740
 Z    =        5046270
71                 I    =           51
86920
 XDOT =      -3957
699876                 Wp   =           51
90512
 YDOT =      -6364
866610  meter/sec      RA   =           47
31147  deg
 ZDOT =      -1791
601098                 TA   =           55
35553
                                          MA   =           55
21665
                                          Ha   =            194
569  n
mi
                                          Hp   =            182
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13986672
95                 X    =        -4300983
20
 Y    =        4004405
42  feet           Y    =         1172657
47  meter
 Z    =       16556006
28                 Z    =         5025468
70
 XDOT =     -12984
579645                 XDOT =       -3877
529462
 YDOT =     -20882
108302  feet/sec       YDOT =       -6408
675379  meter/sec
 ZDOT =      -5877
956359                 ZDOT =       -1810
633849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2221529
46                 X    =         -677122
18
 Y    =       14471250
83  feet           Y    =         4410837
25  meter
 Z    =       16474566
26                 Z    =         5021447
79
 XDOT =     -23322
647072                 XDOT =       -7108
742828
 YDOT =       3243
200470  feet/sec       YDOT =         988
527503  meter/sec
 ZDOT =      -5952
809597                 ZDOT =       -1814
416365


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09148
54460235  
00010596  00000-0  82463-4 0  9102
2 25544  51
6415  47
6809 0009283  50
7023 309
4962 15
73206304  2867


Satellite: ISS
Catalog Number: 25544
Epoch time:      09148
54460235   =   yrday
fracday
Element set:     910
Inclination:       51
6415  deg
RA of node:        47
6809  deg
Eccentricity:     
0009283     
Arg of perigee:    50
7023  deg
Mean anomaly:     309
4962  deg
Mean motion:   15
73206304  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             286
Checksum:              299


Coasting Arc #12 (Orbit 301)
---------------------------------------

Vector Time (GMT): 2009/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4140938
89                 A    =         6733749
66  meter
 Y    =        5133778
21  meter          E    =           
0023291
 Z    =        1298350
26                 I    =           51
88307
 XDOT =      -4507
830112                 Wp   =           57
19221
 YDOT =       2134
105721  meter/sec      RA   =           42
22564  deg
 ZDOT =       5875
532459                 TA   =          317
01874
                                          MA   =          317
20046
                                          Ha   =            194
543  n
mi
                                          Hp   =            182
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13585757
50                 X    =         4076917
21
 Y    =       16843104
35  feet           Y    =         5179726
47  meter
 Z    =        4259679
32                 Z    =         1318312
06
 XDOT =     -14789
468872                 XDOT =       -4559
901202
 YDOT =       7001
659188  feet/sec       YDOT =        2083
404604  meter/sec
 ZDOT =      19276
681297                 ZDOT =        5853
507283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20865133
40                 X    =         6359692
66
 Y    =       -5677568
10  feet           Y    =        -1730522
76  meter
 Z    =        4338117
98                 Z    =         1322258
36
 XDOT =         32
052982                 XDOT =           9
769749
 YDOT =      14936
566152  feet/sec       YDOT =        4552
665363  meter/sec
 ZDOT =      19190
488018                 ZDOT =        5849
260748


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   09149
56096558  
00010596  00000-0  82463-4 0  9119
2 25544  51
6419  42
4674 0009343  54
5786 305
6248 15
73184104  3026


Satellite: ISS
Catalog Number: 25544
Epoch time:      09149
56096558   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:        42
4674  deg
Eccentricity:     
0009343     
Arg of perigee:    54
5786  deg
Mean anomaly:     305
6248  deg
Mean motion:   15
73184104  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             302
Checksum:              315

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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